snrdg082102
SOC-14 1K
To ensure I'm on the right track with Tac Missile design here is what I have for a TL 9 11 cm HE tac missile.
1. Warhead: TL 9 HE weight: 1.75 kg, volume: 0.00175 m^3, price: Cr14
2. Guidance: Operator guided Radio link
A. Warhead guidance package: weight: 2 kg, volume: .002 m^3, price: Cr200
B. Launcher guidance package: weight: 20 kg, volume: .02 m^3, price: Cr2000
C. 5 power radio:, weight: .1 kg, volume: .0002 m^3, price: Cr75
3. Rail Launcher: weight: 1.75 kg, volume: 0.00175 m^3, price: Cr87.5
4. Propellant: 5 power radio has a maximum range of 5 km.
A. Warhead and guidance combined weight = 1.75 + 2 + 0.1 = 3.85 kg
B. Propellant weight multiplier is 3 + 0.1 for being over 4 km.
C. Required propellant weight: 3.85 kg x 3.1 = 11.935 kg
D. Propellant data: weight: 11.935 kg, volume: .011935 m^3, price: Cr11.935
Missile Statistics:
A. Weight: 1.75 + 2 + 0.1 + 11. 935 = 15.785 kg
B. Volume: .00175 + 0.002 + 0.0002 + 0.011935 = 0.015885 m^3
C. Price: 14 + 200 + 75 + 11.935 = Cr300.935
Launcher Statistics:
A. Weight: 1.75 + 20 + 0.1 = 21.85 kg
B. Volume: .00175 + 0.02 + .0002 = 0.02195 m^3
C. Price: 87.5 + 2000 + 75 = Cr2162.5
Total System:
A. Weight: 15.785 + 21.85 = 37.635 kg
B. Volume: .0.015885 + 0.02195 = 0.0237 m^3
C. Price: 300.935 +2162.5 = Cr2463.435
Hopefully my numbers are right too.
Nope, the numbers where a bit off, hopefully my corrections are right, (I'm keeping my fingers crossed
):
Revised calculations changed volume and cost. Radio volume was miss calculated
1. Warhead: TL 9 HE weight: 1.75 kg, volume: 0.00175 m^3, price: Cr14
2. Guidance: Operator guided Radio link
A. Warhead guidance package: weight: 2 kg, volume: .002 m^3, price: Cr200
B. Launcher guidance package: weight: 20 kg, volume: .02 m^3, price: Cr2000
C. 5 power radio:, weight: .1 kg, volume: .0002 m^3, price: Cr75
3. Rail Launcher: weight: 1.75 kg, volume: 0.00175 m^3, price: Cr87.5
4. Propellant: 5 power radio has a maximum range of 5 km.
A. Warhead and guidance combined weight = 1.75 + 2 + 0.1 = 3.85 kg
B. Propellant weight multiplier is 3 + 0.1 for being over 4 km.
C. Required propellant weight: 3.85 kg x 3.1 = 11.935 kg
D. Propellant data: weight: 11.935 kg, volume: .011935 m^3, price: Cr11.935
Missile Statistics:
A. Weight: 1.75 + 2 + 0.1 + 11. 935 = 15.785 kg
B. Volume: .00175 + 0.002 + 0.0002 + 0.011935 = 0.015885 m^3
C. Price: 14 + 200 + 75 + 11.935 = Cr300.935
Launcher Statistics:
A. Weight: 1.75 + 20 + 0.1 = 21.85 kg
B. Volume: .00175 + 0.02 + .0002 = 0.02195 m^3
C. Price: 87.5 + 2000 + 75 = Cr2162.5
Total System:
A. Weight: 15.785 + 21.85 = 37.635 kg
B. Volume: .0.015885 + 0.02195 = 0.0237 m^3
C. Price: 300.935 +2162.5 = Cr2463.435
Hopefully my numbers are right too.
Nope, the numbers where a bit off, hopefully my corrections are right, (I'm keeping my fingers crossed

Revised calculations changed volume and cost. Radio volume was miss calculated
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